Model: 674941

Aircraft G Compressor Blade Lock

Special Features:

Goes on the rear-rotor compressor

Properties:

Overall Length
Between 0.810 inches and 0.820 inches
Overall Width
Between 0.342 inches and 0.349 inches
Material Thickness
Between 0.046 inches and 0.051 inches
End Application
J57 aircraft engine
Criticality Code Justification
Agav
Stage Number
14
Material
Nickel alloy
Material Specification
Pwa1038 assn standard single material response
Reference Data And Literature
2j-j57-14
NSN
2840-00-883-5968
Part Number
674941
Description
Lock,compressor Blade,aircraft G
CAGE
77445

An item used to maintain the position of a blade, compressor, aircraft gas turbine engine in the proper place on a disk, compressor, aircraft gas turbine engine. this item eliminates axial movement of the blade.

Part 674941 NSN 2840-00-883-5968

INC
FIIG
Concept No.
App. Key
Cond. Code
Status
INC:
50454
FIIG:
A503Q0
Concept No.:
App. Key:
Cond. Code:
1
Status:
A

Material Classification

Hazardous material, precious metals, criticality, enviroment, and electrostatic discharge indicators
HMIC
PMIC
ESD/EMI
ENAC
MMAC
CRITL
HMIC:
N
PMIC:
U
ESD:
ESD:
MMAC:
RU
CRITL:
Y

Packaging & Shipping

Est. Pack Size
Est. Pack Weight
Est. Item Weight
Est. Item Dim.
Pack Size:
--
Paclk Weight:
0.1000lbs
Item Weight:
--
Item Dim:
--
OPI
SPI No.
SPI Rev.
SPC Mkg.
LVL A
LVL B
OPI:
O
SPI No.:
SPI Rev.:
SPC Mkg:
00
LVL_A:
E
LVL_B:
Q

Freight Classification

NMFC
UFC
LTL
LCL
WCC
TCC
SHC
ACC
NMFC:
095190
UFC:
49790
LTL:
RATING VARIABLE
LCL:
70.0
WCC:
713
TCC:
Z
SHC:
Z
ACC:
Equipment for Aircraft

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Schedule B and Export
  • Schedule B: 8411997050
  • SITC: 71499
  • End Use: Engines and turbines for military aircraft
  • NAICS: 336412
  • USDA: 1

Freight Class: Parts of gas turbine aircraft engines, other than for use in civil aircraft

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